Nomad II
by Aaron Wigley (wigs@yoyo.cc.monash.edu.au)
Manufacturer: Commonwealth Aerospace Technologies Australia
First available to the public in 2012, the Nomad II is the replacement for the Nomad aircraft, now nearing the end of its operational life. When it was made available, an initial purchase order of 50 was made to the Australian government; since then, almost 2500 aircraft based on the Nomad II were built.
Handling B/A Sig APilot
4 6/4 3 2
Seating: 2 bucket seats Access: 1 midsection large door
options below 1 emergency rear
Takeoff/Landing Profile: STOL
Fuel: 1200 litres in integral wing tanks (1100 kg)
400 litres in wingtip tanks (250 kg)
Powerplant: Two Rolls-Royce turboprop engines, each rated at
430 kW, driving five-blade reversible pitch pusher
propellor.
Systems: Pressurization System, provides cabin altitude of 2000 m
up to 7000 m.
ILS Avionics
GPS
Performance:
Range at 90% power, with 45 minute reserves
1500 km
Econ cruising speed 500 kph
Stalling speed, power off
flaps up 100 kph
flaps down 80 kph
Ceiling 7,000 m
Weights:
Weight Empty, typical 2,000 kg
Max Payload 1,200 kg
Max Fuel Weight 1,300 kg
Max T-O Weight 4,000 kg
Dimensions:
Wing span 15.0 m
Length overall 14 m
Height overall 5.4 m
Options:
Up to 4 underwing hardpoints carrying up to 500 kg loads.
Nose Bay, 10 CF for avionics/electronics.
Removable seat Armour.
>>>>>[ This is a little obsolete by today’s standards, but most airframes still flying are airworthy. The Nomad II was built to land on the roughest strips, day after day, and was also sold to the military. The only difference between the civilian and military releases is the avionics and creature comforts. The airframes are identical. In fact, many south-east Asian countries used these for military operations in support and surveillance operations. ]<<<<<
- True Blue (16:50 30 Nov 2051)
Nomad III
by Aaron Wigley (wigs@yoyo.cc.monash.edu.au)
Manufacturer: Commonwealth Aerospace Technologies Australia
The much-heralded upgrade from the aging Nomad II, the Nomad III is perfect for the rugged use and abuse of the outback of Australia, to coastal duties, or for long-distance airlifting of personnel and materials.
Handling B/A Sig APilot
4 7/2(6) 3 4
Seating: 2 bucket seats Access: 1 midsection large door
options below 1 emergency rear
Takeoff/Landing Profile: STOL
Fuel: 1500 litres in integral wing tanks (1200 kg)
500 litres in wingtip tanks (300 kg)
Powerplant: Two Rolls-Royce turboprop engines, each rated at
500 kW, driving five-blade reversible pitch pusher
propellor.
Systems: Pressurization System, provides cabin altitude of 2000 m
up to 7000 m.
MLS Avionics
GPS
Performance:
Range at 90% power, with 45 minute reserves
1800 km
Econ cruising speed 550 kph
Stalling speed, power off
flaps up 100 kph
flaps down 80 kph
Ceiling 7,000 m
Weights:
Weight Empty, typical 2,300 kg
Max Payload 1,300 kg
Max Fuel Weight 1,500 kg
Max T-O Weight 4,500 kg
Dimensions:
Wing span 16.0 m
Length overall 15 m
Height overall 5.5 m
Options:
Up to 4 underwing hardpoints carrying up to 500 kg loads.
Nose Bay, 10 CF for avionics/electronics.
Removable seat Armour.
>>>>>[ From the people who brought you the Jindevik and Wandjina RPV’s, comes this piece of reliability. She is built to take any punishment, unprepared fields, bad weather, and come out smiling. Like the Nomads before it, it’s a military-grade airframe available to anyone who can afford it, no special licenses needed. Even the Flying Doctors love it. ]<<<<<
- True Blue (20:14 09 Aug 2052)

